The present application relates to a stopping device, a moving mechanism and an aircraft. The moving mechanism is connected to a stationary structure of the aircraft so as to allow the moving mechanism to move relative to the stationary structure. The stopping device includes a first stopper provided at the moving mechanism and a second stopper provided at the stationary structure, and is configured such that when a drive connection structure of the moving mechanism fails, the first stopper is adapted to abut against the second stopper to limit the moving range of the moving mechanism. At least one of the first stopper and the second stopper includes a buffer region made by modifying its meso-structure and thus has a reduced density to thereby be adapted to reduce a dynamic load generated when the first stopper collides with the second stopper.


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    Titel :

    STOPPING DEVICE, MOVING MECHANISM AND AIRCRAFT


    Beteiligte:
    SUN YUMIN (Autor:in)

    Erscheinungsdatum :

    2018-10-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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